Experimental Characterization of Aircraft Electromagnetic Protections
Аннотации
In the paper, an original construction of a coaxial flange for measurements of shielding efficiency of composite materials is presented. The measurement procedure is conceived as a differential method to suppress influence of a flange. Attention is turned to measurements of carbon composites used in aerospace industry. The studied materials exhibit a significant ability to shield electromagnetic radiation. The shielding efficiency is rising with material thickness and with the number of fiber-to-fiber contacts. The optimal composite structure consists of 4 layers of carbon composite; more layers do not influence the shielding efficiency significantly.
Keywords
Carbon composite, carbon-fiber-reinforced polymer (CFRP), glass-fiber composite (GFC), shielding efficiency, measurements, aerospace applications, coaxial flangeDocument type
Peer reviewedDocument version
Final PDFSource
Radioengineering. 2021 vol. 30, č. 4, s. 654-661. ISSN 1210-2512https://www.radioeng.cz/fulltexts/2021/21_04_0654_0661.pdf
Collections
- 2021/4 [18]
Citace PRO
Except where otherwise noted, this item's license is described as Creative Commons Attribution 4.0 International license